View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23687U 95055B 22144.34749273 .00000108 00000-0 16735-2 0 9995
2 23687 4.8753 97.0847 7245070 310.3217 6.1324 2.21811793215066
| Epoch (UTC): | 24 May 2022 08:20:23 |
| Eccentricity: | 0.7245070 |
| inclination: | 4.8753° |
| perigee height: | 464 km |
| apogee height: | 36451 km |
| right ascension of ascending node: | 97.0847° |
| argument of perigee: | 310.3217° |
| revolutions per day: | 2.21811793 |
| mean anomaly at epoch: | 6.1324° |
| orbit number at epoch: | 21506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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